Hellow courtneywetts,
courtneywetts said:
The asteroid is twice as far from the Sun as Earth, so it receives ¼ the solar energy. Thus
T = [341 W/m2 (1 – 0.15)/(4 5.67e-8 W/(m2 K4))]1/4 = 189 KI know this is right because my professor did this as a solution but I am confused as how this was reached.
Which part of the solution are you confused about?
As you stated, since the asteroid is twice the distance of Earth from the sun, it receives 1/4 of the power per unit area. This is because of the
inverse-square law for the intensity of light. So that's where the 341 W/m
2 comes from (we receive 4 times that amount of solar energy at the surface of the Earth, roughly).
The (1 - 0.15) is because of the albedo. An albedo of 0.15 means that 15% of the incoming light is reflected back into space. This means that 85% of it (1 - 0.15) is absorbed, heating up the asteroid. Hence, we multiply the incoming solar radiation by this factor, to get the actual amount absorbed.
Next, comes the only tricky part, conceptually. What you have to realize is that if the asteroid is in thermal equilibrium, then the energy coming in in the form of EM radiation must be equal to the energy going out. In other words, the asteroid re-radiates all of the solar energy that it receives back into space. If this were not true, and the input were not the same as the output, the asteroid would heat up or cool down
until this equilibrium was reached.
So, for the final part of the problem, you assume that the asteroid is itself a blackbody emitter, and apply the Stefan-Boltzmann law to it:$$P/A = \sigma T^4$$where you know what P/A is, it's just 0.85*(341 W/m
2) (since it has to re-emit all of the solar power that it absorbs).
Your professor solved this equation for T.